US4366108A - Liquid matrix system based on a mixture of epoxide resin and an amine curing agent for producing fibre-reinforced plastics components - Google Patents

Liquid matrix system based on a mixture of epoxide resin and an amine curing agent for producing fibre-reinforced plastics components Download PDF

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Publication number
US4366108A
US4366108A US06/283,766 US28376681A US4366108A US 4366108 A US4366108 A US 4366108A US 28376681 A US28376681 A US 28376681A US 4366108 A US4366108 A US 4366108A
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weight
matrix system
percent
component
mixture
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Expired - Fee Related
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US06/283,766
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English (en)
Inventor
Karl Urech
Jurgen Habermeier
Roland Moser
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Novartis Corp
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Ciba Geigy Corp
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Assigned to CIBA-GEIGY CORPORATION, A CORP. OF N.Y. reassignment CIBA-GEIGY CORPORATION, A CORP. OF N.Y. ASSIGNMENT OF ASSIGNORS INTEREST. Assignors: CIBA-GEIGY AG. A SWISS COMPANY
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    • CCHEMISTRY; METALLURGY
    • C08ORGANIC MACROMOLECULAR COMPOUNDS; THEIR PREPARATION OR CHEMICAL WORKING-UP; COMPOSITIONS BASED THEREON
    • C08JWORKING-UP; GENERAL PROCESSES OF COMPOUNDING; AFTER-TREATMENT NOT COVERED BY SUBCLASSES C08B, C08C, C08F, C08G or C08H
    • C08J5/00Manufacture of articles or shaped materials containing macromolecular substances
    • C08J5/04Reinforcing macromolecular compounds with loose or coherent fibrous material
    • CCHEMISTRY; METALLURGY
    • C08ORGANIC MACROMOLECULAR COMPOUNDS; THEIR PREPARATION OR CHEMICAL WORKING-UP; COMPOSITIONS BASED THEREON
    • C08GMACROMOLECULAR COMPOUNDS OBTAINED OTHERWISE THAN BY REACTIONS ONLY INVOLVING UNSATURATED CARBON-TO-CARBON BONDS
    • C08G59/00Polycondensates containing more than one epoxy group per molecule; Macromolecules obtained by polymerising compounds containing more than one epoxy group per molecule using curing agents or catalysts which react with the epoxy groups
    • C08G59/18Macromolecules obtained by polymerising compounds containing more than one epoxy group per molecule using curing agents or catalysts which react with the epoxy groups ; e.g. general methods of curing
    • C08G59/40Macromolecules obtained by polymerising compounds containing more than one epoxy group per molecule using curing agents or catalysts which react with the epoxy groups ; e.g. general methods of curing characterised by the curing agents used
    • C08G59/50Amines
    • C08G59/5033Amines aromatic
    • CCHEMISTRY; METALLURGY
    • C08ORGANIC MACROMOLECULAR COMPOUNDS; THEIR PREPARATION OR CHEMICAL WORKING-UP; COMPOSITIONS BASED THEREON
    • C08JWORKING-UP; GENERAL PROCESSES OF COMPOUNDING; AFTER-TREATMENT NOT COVERED BY SUBCLASSES C08B, C08C, C08F, C08G or C08H
    • C08J2363/00Characterised by the use of epoxy resins; Derivatives of epoxy resins

Definitions

  • Epoxide resin/curing agent systems which can be used for producing fibre-reinforced plastics, such as laminates, are known. It is of advantage for impregnating the fibres when these systems are liquid and of low viscosity, and for this reason the systems contain liquid acid anhydrides as curing agents. After prolonged contact with water, cured composites produced from a system of this type commence to decompose as a result of hydrolysis, a disadvantage which, as is known, epoxide resin systems with aromatic amine curing agents do not have. Systems of this kind, however, are solid and/or cure only at very high temperatures. The curing temperature can indeed be lowered by the addition of accelerators, but there is a simultaneous shortening of the pot life, so that such systems are not suitable for carrying out filament winding or pultrusion on an industrial scale.
  • the invention relates therefore to a liquid matrix system, based on a mixture of epoxide resin and an amine curing agent for the epoxide resin, for producing fibre-reinforced plastics components, which system is characterised in that it has at 40° C. a dynamic viscosity of less than 400 mPa s, preferably less than 250 mPa s, and contains
  • Polyglycidyl compounds (a) are preferably those based on bisphenol-F or on bisphenol-A, or based on phenolnovolaks, or on mixtures thereof in any mixture ratio. They can be mixed with a polyglycide of an alkanediol, such as butanediol diglycide, preferably in an amount of 3-5 percent by weight, relative to the total amount of the polyglycidyl compounds, or with an aromatic compound having amino and hydroxyl groups, such as diglycidyl-p-aminophenol, preferably in an amount of 3-20 percent by weight, relative to the total amount of polyglycidyl compounds.
  • an alkanediol such as butanediol diglycide
  • an aromatic compound having amino and hydroxyl groups such as diglycidyl-p-aminophenol
  • polyglycidyl compounds are triglycidyl-p-aminophenol and tetraglycidyl-p,p'-diaminodiphenylmethane, which can be mixed with butanediol diglycide or triglycidyl-p-aminophenol.
  • the compounds mentioned can also be used in any admixtures with one another or with hydantoin diglycidyl compounds, such as N,N'-diglycidyl-5,5-dimethylhydantoin, provided that the viscosity of the final mixture at 40° C. is less then 400 mPa s.
  • the accelerator (c) is advantageously mixed with diethyltoluylenediamine (mostly 1-methyl-3,5-diethyl-2,4-diaminobenzene, but also 1-methyl-3,5-diethyl-2,6-diaminobenzene) in a quantitative ratio within the stated range.
  • Suitable accelerators are tertiary amines, for example 1-methyl-imidazole, or phenols, such as salicylic acid, especially however borofluoroamine complexes of organic compounds, such as BF 2 -acetoacetanilide, BF 3 -aniline complexes or BF 3 -monoethylamine.
  • the component (b) having at all events to be present to the extent of at least 50 percent by weight in the mixture (b)+(c)+(d).
  • the matrix system according to the invention is preferably applied without solvent. It can however contain, relative to the total weight of the matrix system, up to 20% of an inert solvent, such as toluene, also up to 20% of a reactive vinyl or acrylic polymer with the corresponding radical initiators, up to 5% of an adhesion promoter and up to 2% of a dye.
  • an inert solvent such as toluene
  • a reactive vinyl or acrylic polymer with the corresponding radical initiators up to 5% of an adhesion promoter and up to 2% of a dye.
  • the matrix system according to the invention preferably contains a mixture of diglycidyl ether of bisphenol-F and bisphenol-A, the epoxide content being 5.3-6.1 val/kg, and, relative to the total amount of glycidyl compounds, 3-15 percent by weight of diglycidyloxybutane or 3-20 percent by weight of triglycidyl-p-aminophenol, as well as (b) a mixture of 95-98 percent by weight of diethyltoluylenediamine and 2-5 percent by weight of BF 2 -acetoacetanilide.
  • This mixture preferably has at 40° C. a dynamic viscosity of less than 250 mPa s.
  • a matrix system which contains as component (a) a mixture of 65 percent by weight of diglycidyl ether of bisphenol-F (epoxide content: 5.8-6.1 val/kg), 30 percent by weight of diglycidyl ether of bisphenol-A (epoxide content: 5.3-6.7 val/kg) and 5 percent by weight of diglycidyloxybutane (epoxide content: 8.5-9.5 val/kg), and, as components (b) and (c), a mixture of 96 percent by weight of diethyltoluylenediamine and 4 percent by weight of difluoroboroacetoacetanilide.
  • component (a) a mixture of 65 percent by weight of diglycidyl ether of bisphenol-F (epoxide content: 5.8-6.1 val/kg), 30 percent by weight of diglycidyl ether of bisphenol-A (epoxide content: 5.3-6.7 val/kg) and 5 percent by weight of diglycidyloxybutan
  • the matrix according to the invention is used to produce fibre-reinforced plastics. It is thus possible, using known impregnating methods, to impregnate and cure fibre materials such as filaments, rovings, mats or fabrics. Advantageous factors in the procedure are the low viscosity at the working temperatures (at 40°-60° C.), the long pot life and the short gelling and curing times.
  • the cured components have good mechanical strengths, high glass transition temperatures and very high thermal stability. Furthermore, their stability in water and resistance to chemicals, particularly at elevated temperatures and after prolonged periods of time, are better than in the case of resin/anhydride curing agent systems, which likewise are systems having low viscosity.
  • the matrix of the invention is suitable for producing prepegs, especially where the operations are performed without solvents, and for use in the pultrusion process, in which the procedure can be carried out with or without solvents; in addition, the matrix is particularly advantageous in those technical fields of operation where solvents have to be avoided, such as in the case of injection moulding or in particular filament winding for producing high-strength, thermally and chemically resistant structural components in large-scale series production.
  • the matrix according to the invention can be employed for example for manufacturing hollow objects, for instance tubes capable of withstanding pressure and torsional stress, such as tubes for universal-joint shafts, stabilisers and axles, and also for producing fibre-reinforced solid materials, for example spring elements.
  • the process for producing fibre-reinforced plastics components which process comprises using the matrix system for impregnating fibre material, forming shaped articles by filament winding or pultrusion and subsequently heating the shaped components at 100°-180° C., especially at 100°-140° C., is likewise subject matter of the present invention.
  • Suitable fibre materials are preferably glass fibres, for example those formed from E- or S-glass, aramid fibres, high-modulus and high-strength carbon fibres made from polyacrylonitrile or pitch, and also polyester and polyamide fibres.
  • the content of fibre material in the cured final product varies depending on the method of production and on the nature of the fibres, for example in a product formed by filament winding the content is between 45 and 75 percent by volume.
  • filament winding precision winding
  • precision winding an operation whereby prestretched, parallel running fibres, impregnated in a resin/curing agent system, are wound round a mandrel, the fibres being located according to a precisely predetermined geometrical pattern.
  • the pultrusion process has similar features. In this case, however, the impregnated rovings are shaped by being pulled through a heated dye and pre-cured to the extent that subsequent curing in a through-type oven can no longer lead to deformation or delamination.
  • a matrix system having a dynamic viscosity of 220 mPa s at 40° C. is thus obtained.
  • the product has a glass transition temperature (T G ) of 168° C. after curing for 8 hours at 140° C., and a T G of 169° C. after curing for 4 hours at 180° C.
  • the matrix system is used for impregnating fibres made from glass, carbon and aramid, from which are produced, by the filament winding process, unidirectional specimens which are subjected, according to W. Knappe and W. Schneider: "Rupture criteria for unidirectional glass-fibre plastics under plane short- and long-duration stressing" in Kunststoffe (Plastics) 62, No. 12, 1972, to the tensile, compression and torsion tests.
  • 75 parts by weight of polyglycidyl ether of epoxyphenol novolak (epoxide content: 5.7 val/kg) and 25 parts by weight of 1,4-butanediol-diglycidyl ether (epoxide content: 9.2 val/kg) are homogeneously mixed together.
  • Into the mixture are stirred 30 parts by weight of a mixture of 83 parts by weight of 1-methyl-3,5-diethyl-2,4-diaminobenzene and 13 parts by weight of p,p'-diamino-diphenylmethane and 4 parts by weight of BF 2 -acetoacetanilide.
  • T G glass transition temperature
  • the tensile strength determined perpendicularly to the fibres on wound objects reinforced unidirectionally with 65% v/v of glass fibres "Cosmostrand 859 ⁇ 29/890"® is 54 N/mm 2 .
  • the matrix system obtained has at 50° C. a dynamic viscosity of 193 mPa s.
  • the product has a T G of 178° C. after a curing time of 8 hours at 140° C.
  • the boiling-water absorption, according to ISO R 117, after 1 hour is 0.24%.

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  • Chemical & Material Sciences (AREA)
  • Health & Medical Sciences (AREA)
  • Chemical Kinetics & Catalysis (AREA)
  • Medicinal Chemistry (AREA)
  • Polymers & Plastics (AREA)
  • Organic Chemistry (AREA)
  • Engineering & Computer Science (AREA)
  • Manufacturing & Machinery (AREA)
  • Materials Engineering (AREA)
  • Reinforced Plastic Materials (AREA)
  • Epoxy Resins (AREA)
  • Compositions Of Macromolecular Compounds (AREA)
US06/283,766 1980-07-25 1981-07-16 Liquid matrix system based on a mixture of epoxide resin and an amine curing agent for producing fibre-reinforced plastics components Expired - Fee Related US4366108A (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
CH570780 1980-07-25
CH5707/80 1980-07-25

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US4366108A true US4366108A (en) 1982-12-28

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Country Status (6)

Country Link
US (1) US4366108A (fr)
JP (1) JPS5751719A (fr)
CA (1) CA1175196A (fr)
DE (1) DE3129016A1 (fr)
FR (1) FR2487371B1 (fr)
GB (1) GB2093034B (fr)

Cited By (20)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4447586A (en) * 1983-04-11 1984-05-08 Celanese Corporation Metal fluoborate catalyzed hindered aromatic amine curing agents for polyepoxide resins
US4528305A (en) * 1984-04-13 1985-07-09 Ciba-Geigy Corporation Epoxy resin modeling stock
US4874833A (en) * 1988-08-22 1989-10-17 Shell Oil Company Composition containing epoxy resin and alkyl hindered polyaromatic diamine and monoaromatic amine curing agents
US5128433A (en) * 1991-06-04 1992-07-07 Polytek Development Corp. Thixotropic polymer compositions and process for use thereof
US5393806A (en) * 1991-12-26 1995-02-28 Albemarle Corporation Epoxide system curing agents
US5482664A (en) * 1991-03-06 1996-01-09 L'amy S.A. Method of manufacturing a synthetic resin spectacle frame component
US5503936A (en) * 1994-02-28 1996-04-02 Ciba-Geigy Corporation N-alkyl-N'-aryl-P-phenylenediamines as modifiers for epoxy resins
US5545278A (en) * 1989-10-25 1996-08-13 Thiokol Corporation Method for increasing fiber strength translation in composition pressure vessels using matrix resin formulations containing anhydride curing agents and surface-active agents
US5585453A (en) * 1982-07-14 1996-12-17 The United States Of America As Represented By The Secretary Of The Army Composite motor case polymers that expand on polymerization
US5593770A (en) * 1989-10-25 1997-01-14 Thiokol Corporation Chemorheologically tailored matrix resin formulations containing anhydride curing agents
US6187443B1 (en) 1996-09-30 2001-02-13 Institut Francais Du Petrole Thermosetting composition, uses thereof and a flexible deployable preform comprising the composition
WO2001042330A1 (fr) * 1999-12-13 2001-06-14 Mitsubishi Rayon Co., Ltd. Composition de resine epoxyde et materiau composite renforce par des fibres constituees de la composition de resine epoxyde
US6410127B1 (en) * 1999-03-11 2002-06-25 Toray Industries, Inc. Epoxy resin compositions, epoxy resin compositions for fiber-reinforced composite materials, and fiber-reinforced composite materials comprising the same
FR2822100A1 (fr) * 2001-03-13 2002-09-20 Inst Francais Du Petrole Methode de fabrication en grande longueur d'elements tubulaires en composite
US6583528B2 (en) * 2000-06-19 2003-06-24 Indigo Energy, Inc. High performance composite flywheel
US6632881B1 (en) * 1999-04-13 2003-10-14 Hitachi Chemical Co., Ltd. Encapsulant of epoxy resin and liquid aromatic amine curing agent
US20040227255A1 (en) * 2003-05-12 2004-11-18 Kazuaki Sumita Liquid epoxy resin composition and flip chip semiconductor device
US20040247882A1 (en) * 2001-11-07 2004-12-09 Shinji Kouchi Epoxy resin compositions for fiber-reinforced composite materials, process for production of the materials and fiber-reinforced composite materials
WO2006129014A2 (fr) * 2005-06-01 2006-12-07 Arkema France Utilisation d'une composition particuliere pour la fabrication de pieces par enroulement filamentaire
US20070238226A1 (en) * 2000-06-30 2007-10-11 Lowrey Tyler A Three dimensional programmable device and method for fabricating the same

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* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
ZA84548B (en) * 1983-05-20 1984-12-24 Union Carbide Corp Impact resistant matrix resins for advanced composites
US4540750A (en) * 1984-09-24 1985-09-10 Ciba-Geigy Corporation Diethyl toluene diamine hardener systems
US6369164B1 (en) 1993-05-26 2002-04-09 Dentsply G.M.B.H. Polymerizable compounds and compositions
US6353061B1 (en) 1993-05-26 2002-03-05 Dentsply Gmbh α, ω-methacrylate terminated macromonomer compounds
US5624976A (en) * 1994-03-25 1997-04-29 Dentsply Gmbh Dental filling composition and method
US5998499A (en) 1994-03-25 1999-12-07 Dentsply G.M.B.H. Liquid crystalline (meth)acrylate compounds, composition and method
CA2146816A1 (fr) 1994-04-22 1995-10-23 Joachim E. Klee Methode et composition pour la preparation d'un produit polymerique dentaire
JP6812672B2 (ja) * 2015-06-25 2021-01-13 東レ株式会社 エポキシ樹脂組成物、繊維強化複合材料、成形品および圧力容器

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GB1034790A (en) 1962-12-28 1966-07-06 Bayer Ag Method of hardening epoxy resins
US3793247A (en) * 1970-08-11 1974-02-19 Ciba Geigy Ag Curable epoxide resin compositions containing boron-trichloride-tertiary amine complexes

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JPS5611964B2 (fr) * 1974-03-25 1981-03-18
JPS5397096A (en) * 1977-02-03 1978-08-24 Kanto Jidosha Kogyo Kk Epoxy resin sheet compound for molding

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GB1034790A (en) 1962-12-28 1966-07-06 Bayer Ag Method of hardening epoxy resins
US3793247A (en) * 1970-08-11 1974-02-19 Ciba Geigy Ag Curable epoxide resin compositions containing boron-trichloride-tertiary amine complexes

Non-Patent Citations (1)

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Title
Lee et al., Handbook of Epoxy Resins, pp. 11-11. *

Cited By (33)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5585453A (en) * 1982-07-14 1996-12-17 The United States Of America As Represented By The Secretary Of The Army Composite motor case polymers that expand on polymerization
EP0122149A2 (fr) 1983-04-11 1984-10-17 INTEREZ, Inc. (a Georgia corporation) Agents de durcissement à base d'amine aromatique à encombrement stérigue, catalysés par un fluoborate métallique, pour résines époxydes
US4447586A (en) * 1983-04-11 1984-05-08 Celanese Corporation Metal fluoborate catalyzed hindered aromatic amine curing agents for polyepoxide resins
US4528305A (en) * 1984-04-13 1985-07-09 Ciba-Geigy Corporation Epoxy resin modeling stock
US4874833A (en) * 1988-08-22 1989-10-17 Shell Oil Company Composition containing epoxy resin and alkyl hindered polyaromatic diamine and monoaromatic amine curing agents
US5545278A (en) * 1989-10-25 1996-08-13 Thiokol Corporation Method for increasing fiber strength translation in composition pressure vessels using matrix resin formulations containing anhydride curing agents and surface-active agents
US5593770A (en) * 1989-10-25 1997-01-14 Thiokol Corporation Chemorheologically tailored matrix resin formulations containing anhydride curing agents
US5482664A (en) * 1991-03-06 1996-01-09 L'amy S.A. Method of manufacturing a synthetic resin spectacle frame component
US5128433A (en) * 1991-06-04 1992-07-07 Polytek Development Corp. Thixotropic polymer compositions and process for use thereof
US5393806A (en) * 1991-12-26 1995-02-28 Albemarle Corporation Epoxide system curing agents
US5503936A (en) * 1994-02-28 1996-04-02 Ciba-Geigy Corporation N-alkyl-N'-aryl-P-phenylenediamines as modifiers for epoxy resins
US6187443B1 (en) 1996-09-30 2001-02-13 Institut Francais Du Petrole Thermosetting composition, uses thereof and a flexible deployable preform comprising the composition
US6485834B1 (en) 1996-09-30 2002-11-26 Institut Francais Du Petrole Flexible deployable preform
US6410127B1 (en) * 1999-03-11 2002-06-25 Toray Industries, Inc. Epoxy resin compositions, epoxy resin compositions for fiber-reinforced composite materials, and fiber-reinforced composite materials comprising the same
US6632881B1 (en) * 1999-04-13 2003-10-14 Hitachi Chemical Co., Ltd. Encapsulant of epoxy resin and liquid aromatic amine curing agent
US20030065095A1 (en) * 1999-12-13 2003-04-03 Takashi Kaneko Epoxy resin composition and fiber-reinforced composite material formed with the epoxy resin composition
US7230052B2 (en) 1999-12-13 2007-06-12 Mitsubishi Rayon Co., Ltd. Epoxy resin composition and fiber reinforced composite material using epoxy resin composition
WO2001042330A1 (fr) * 1999-12-13 2001-06-14 Mitsubishi Rayon Co., Ltd. Composition de resine epoxyde et materiau composite renforce par des fibres constituees de la composition de resine epoxyde
US6875825B2 (en) * 1999-12-13 2005-04-05 Mitsubishi Rayon Co., Ltd. Composition of bisphenol or novolak epoxy resin, epoxy resin from monoaromatic backbone and aromatic amine
US20050101748A1 (en) * 1999-12-13 2005-05-12 Mitsubishi Rayon Co., Limited Epoxy resin composition and fiber reinforced composite material using epoxy resin composition
US6583528B2 (en) * 2000-06-19 2003-06-24 Indigo Energy, Inc. High performance composite flywheel
US7566646B2 (en) 2000-06-30 2009-07-28 Intel Corporation Three dimensional programmable device and method for fabricating the same
US20070238226A1 (en) * 2000-06-30 2007-10-11 Lowrey Tyler A Three dimensional programmable device and method for fabricating the same
FR2822100A1 (fr) * 2001-03-13 2002-09-20 Inst Francais Du Petrole Methode de fabrication en grande longueur d'elements tubulaires en composite
US20080108761A1 (en) * 2001-11-07 2008-05-08 Shinji Kouchi Epoxy resin composition for fiber reinforced composite material, a production method for fiber reinforced composite material, and a fiber reinforced composite material
US20040247882A1 (en) * 2001-11-07 2004-12-09 Shinji Kouchi Epoxy resin compositions for fiber-reinforced composite materials, process for production of the materials and fiber-reinforced composite materials
US7709582B2 (en) * 2001-11-07 2010-05-04 Toray Industries, Inc. Epoxy resin composition for fiber reinforced composite material, a production method for fiber reinforced composite material, and a fiber reinforced composite material
US20100151137A1 (en) * 2001-11-07 2010-06-17 Toray Industries, Inc. Epoxy resin composition for fiber reinforced composite material, a production method for fiber reinforced composite material, and a fiber reinforced composite material
US20090184431A1 (en) * 2003-05-12 2009-07-23 Shin-Etsu Chemical Co., Ltd. Liquid epoxy resin composition and flip chip semiconductor device
US20040227255A1 (en) * 2003-05-12 2004-11-18 Kazuaki Sumita Liquid epoxy resin composition and flip chip semiconductor device
WO2006129014A3 (fr) * 2005-06-01 2007-01-25 Arkema France Utilisation d'une composition particuliere pour la fabrication de pieces par enroulement filamentaire
FR2886644A1 (fr) * 2005-06-01 2006-12-08 Arkema Sa Utilisation d'une composition particuliere pour la fabrication de pieces par enroulement filamentaire
WO2006129014A2 (fr) * 2005-06-01 2006-12-07 Arkema France Utilisation d'une composition particuliere pour la fabrication de pieces par enroulement filamentaire

Also Published As

Publication number Publication date
JPS5751719A (en) 1982-03-26
GB2093034B (en) 1984-04-04
DE3129016A1 (de) 1982-03-18
FR2487371B1 (fr) 1986-04-11
FR2487371A1 (fr) 1982-01-29
GB2093034A (en) 1982-08-25
CA1175196A (fr) 1984-09-25

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